Three-dimensional Stability Analysis of Piezoelectric Antisymmetric Angle-Ply Laminates Using Finite Layer Method

被引:10
作者
Akhras, G. [1 ]
Li, W. C. [1 ]
机构
[1] Royal Mil Coll Canada, Ctr Smart Mat & Struct, Kingston, ON K7K 7B4, Canada
关键词
3D stability analysis; anti-symmetric angle-ply; finite layer method; COUPLED MECHANICS; COMPOSITE; PLATES;
D O I
10.1177/1045389X10364865
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
The finite layer method is the most efficient numerical method for 3D analysis of simply supported rectangular plates. In this method, the plate is divided into a number of finite layers. Within each finite layer, trigonometric functions are used for the in-plane interpolations of displacements, whereas polynomials are employed for the interpolations in the thickness direction. Thus, the 3D analysis is transformed into a series of 1D analyses, and the efficiency is enhanced significantly. In the present study, the finite layer method is extended to the stability analysis of piezoelectric antisymmetric angle-ply laminates, which may be also combined with some symmetrical cross-plies. Numerical results are presented to verify the proposed method. The effects of side-to-thickness ratio, aspect ratio, number of plies, fiber-orientation, and electrical conditions on stability behaviors of some piezoelectric laminates are investigated.
引用
收藏
页码:719 / 727
页数:9
相关论文
共 14 条
[1]   Three-dimensional static, vibration and stability analysis of piezoelectric composite plates using a finite layer method [J].
Akhras, G. ;
Li, W. C. .
SMART MATERIALS & STRUCTURES, 2007, 16 (03) :561-569
[2]   Three-dimensional thermal buckling analysis of piezoelectric composite plates using the finite layer method [J].
Akhras, G. ;
Li, W. C. .
SMART MATERIALS AND STRUCTURES, 2008, 17 (05)
[3]  
Cheung M.S., 1996, Finite Strip Analysis of Bridges
[4]   Finite layer method in analyses of piezoelectric composite laminates [J].
Cheung, YK ;
Jiang, CP .
COMPUTER METHODS IN APPLIED MECHANICS AND ENGINEERING, 2001, 191 (8-10) :879-901
[5]   BUCKLING OF RECTANGULAR MINDLIN PLATES [J].
DAWE, DJ ;
ROUFAEIL, OL .
COMPUTERS & STRUCTURES, 1982, 15 (04) :461-471
[6]   Thermal, electrical, mechanical coupled mechanics for initial buckling analysis of smart plates and beams using discrete layer kinematics [J].
Giannopoulos, G. ;
Santafe, F. ;
Monreal, J. ;
Vantomme, J. .
INTERNATIONAL JOURNAL OF SOLIDS AND STRUCTURES, 2007, 44 (14-15) :4707-4722
[7]   Analytical solutions for free vibration of laminated composite and sandwich plates based on a higher-order refined theory [J].
Kant, T ;
Swaminathan, K .
COMPOSITE STRUCTURES, 2001, 53 (01) :73-85
[8]   Nonlinear coupled zigzag theory for buckling of hybrid piezoelectric plates [J].
Kapuria, S. ;
Achary, G. G. S. .
COMPOSITE STRUCTURES, 2006, 74 (03) :253-264
[9]   Exact 3-D piezoelasticity solution for buckling of hybrid cross-ply plates using transfer matrices [J].
Kapuria, S ;
Achary, GGS .
ACTA MECHANICA, 2004, 170 (1-2) :25-45
[10]   3-DIMENSIONAL SOLUTIONS FOR THERMAL BUCKLING OF MULTILAYERED ANISOTROPIC PLATES [J].
NOOR, AK ;
BURTON, WS .
JOURNAL OF ENGINEERING MECHANICS-ASCE, 1992, 118 (04) :683-701